The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 29, 2019

Filed:

Dec. 09, 2015
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Kok-Mun Tham, Oviedo, FL (US);

Ching-Pang Lee, Cincinnati, OH (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 11/12 (2006.01); F04D 29/68 (2006.01); B22D 25/02 (2006.01); F01D 5/18 (2006.01); C23C 4/02 (2006.01); C23C 4/18 (2006.01); C23C 28/00 (2006.01); C23C 4/073 (2016.01); F04D 29/52 (2006.01); B22C 7/02 (2006.01); B22C 9/24 (2006.01); B22D 29/00 (2006.01); F01D 9/02 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
B22D 25/02 (2013.01); B22C 7/02 (2013.01); B22C 9/24 (2013.01); B22D 29/001 (2013.01); C23C 4/02 (2013.01); C23C 4/073 (2016.01); C23C 4/18 (2013.01); C23C 28/3215 (2013.01); C23C 28/3455 (2013.01); F01D 5/18 (2013.01); F01D 5/186 (2013.01); F01D 11/08 (2013.01); F01D 11/122 (2013.01); F01D 11/127 (2013.01); F04D 29/526 (2013.01); F04D 29/685 (2013.01); F01D 5/187 (2013.01); F01D 9/023 (2013.01); F01D 25/12 (2013.01); F05D 2220/32 (2013.01); F05D 2230/00 (2013.01); F05D 2230/211 (2013.01); F05D 2230/30 (2013.01); F05D 2230/90 (2013.01); F05D 2240/11 (2013.01); F05D 2250/12 (2013.01); F05D 2250/15 (2013.01); F05D 2250/182 (2013.01); F05D 2250/183 (2013.01); F05D 2250/184 (2013.01); F05D 2250/185 (2013.01); F05D 2250/23 (2013.01); F05D 2250/282 (2013.01); F05D 2250/292 (2013.01); F05D 2250/294 (2013.01); F05D 2250/60 (2013.01); F05D 2250/75 (2013.01); F05D 2260/202 (2013.01); F05D 2260/22141 (2013.01); F05D 2300/175 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

Turbine and compressor casing abradable components for turbine engines include abradable surfaces with a zonal system of forward (zone A) and rear or aft sections (zone B) surface features. The zone A surface profile comprises an array pattern of non-directional depression dimples, or upwardly projecting dimples, or both, in the abradable surface. The dimpled forward zone A surface features reduce surface solidity in a controlled manner, to help increase abradability during blade tip rubbing incidents, yet they provide sufficient material to resist incoming hot working fluid erosion of the abradable surface. In addition, the dimples provide generic forward section aerodynamic profiling to the abradable surface, compatible with different blade airfoil-camber profiles. The aft zone B surface features comprise an array pattern of ridges and grooves.


Find Patent Forward Citations

Loading…